ES3061514T3 - Hypersonic transport system - Google Patents
Hypersonic transport systemInfo
- Publication number
- ES3061514T3 ES3061514T3 ES22714486T ES22714486T ES3061514T3 ES 3061514 T3 ES3061514 T3 ES 3061514T3 ES 22714486 T ES22714486 T ES 22714486T ES 22714486 T ES22714486 T ES 22714486T ES 3061514 T3 ES3061514 T3 ES 3061514T3
- Authority
- ES
- Spain
- Prior art keywords
- aircraft
- propulsion device
- control unit
- descent
- transport system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
- B64G1/006—Reusable launch rockets or boosters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Tires In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2102867A FR3121125B1 (fr) | 2021-03-23 | 2021-03-23 | Système de transport hypersonique |
| PCT/FR2022/050484 WO2022200713A1 (fr) | 2021-03-23 | 2022-03-17 | Systeme de transport hypersonique |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES3061514T3 true ES3061514T3 (en) | 2026-04-06 |
Family
ID=76807709
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES22714486T Active ES3061514T3 (en) | 2021-03-23 | 2022-03-17 | Hypersonic transport system |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20250074588A1 (de) |
| EP (1) | EP4313762B1 (de) |
| ES (1) | ES3061514T3 (de) |
| FR (1) | FR3121125B1 (de) |
| WO (1) | WO2022200713A1 (de) |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6257527B1 (en) * | 1997-11-10 | 2001-07-10 | Fred Whitney Redding, Jr. | Hypersonic and orbital vehicles system |
| US6634594B1 (en) * | 2002-05-03 | 2003-10-21 | The Boeing Company | Hypersonic waverider variable leading edge flaps |
| US6745979B1 (en) * | 2002-10-22 | 2004-06-08 | Zhuo Chen | Spacecraft and aerospace plane having scissors wings |
| EP2151730A1 (de) * | 2008-08-05 | 2010-02-10 | The Boeing Company | Vierdimensionale Flugzeugnavigation |
| WO2010148025A1 (en) * | 2009-06-15 | 2010-12-23 | Blue Origin, Llc | Compensating for wind prior to engaging airborne propulsion devices |
| US8729442B2 (en) * | 2009-06-15 | 2014-05-20 | Blue Origin, Llc | Predicting and correcting trajectories |
| US8955791B2 (en) * | 2012-05-10 | 2015-02-17 | The Boeing Company | First and second stage aircraft coupled in tandem |
| JP6720031B2 (ja) * | 2016-09-08 | 2020-07-08 | 三菱重工業株式会社 | 宇宙機及びその着陸方法 |
| EP3532901B1 (de) * | 2016-10-28 | 2022-08-17 | Booz Allen Hamilton Inc. | Fahrzeugleitsystem und verfahren, das luftdaten aus oberflächenmontierten drucksensoren zur fahrzeugausrichtungssteuerung nutzt |
| US10669047B2 (en) * | 2017-05-24 | 2020-06-02 | The Boeing Company | System and method for hypersonic payload separation |
| CN107985626B (zh) * | 2017-10-27 | 2021-02-19 | 南京航空航天大学 | 一种基于可变构型空天飞行器的气动布局设计方法 |
| US11053018B2 (en) * | 2018-06-27 | 2021-07-06 | Raytheon Company | Flight vehicle engine inlet with internal diverter, and method of configuring |
| JP7413121B2 (ja) * | 2020-03-27 | 2024-01-15 | 三菱重工業株式会社 | 滑空制御装置、滑空体、飛行体、および滑空プログラム |
| US12017807B2 (en) * | 2020-06-17 | 2024-06-25 | Jasem Jamal Alhubail | Apparatus, systems and methods for controlling a spacecraft during atmospheric reentry |
| US12092432B2 (en) * | 2020-10-02 | 2024-09-17 | United States Of America, As Represented By The Secretary Of The Navy | Glide trajectory optimization for aerospace vehicles |
-
2021
- 2021-03-23 FR FR2102867A patent/FR3121125B1/fr active Active
-
2022
- 2022-03-17 EP EP22714486.2A patent/EP4313762B1/de active Active
- 2022-03-17 ES ES22714486T patent/ES3061514T3/es active Active
- 2022-03-17 US US18/551,499 patent/US20250074588A1/en active Pending
- 2022-03-17 WO PCT/FR2022/050484 patent/WO2022200713A1/fr not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| EP4313762C0 (de) | 2025-11-05 |
| FR3121125A1 (fr) | 2022-09-30 |
| FR3121125B1 (fr) | 2024-05-03 |
| WO2022200713A1 (fr) | 2022-09-29 |
| EP4313762B1 (de) | 2025-11-05 |
| US20250074588A1 (en) | 2025-03-06 |
| EP4313762A1 (de) | 2024-02-07 |
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